A model of instability of liquid propellant engine with radial injection-Reference-Cited by-同舟云学术

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A model of instability of liquid propellant engine with radial injection

Published:1982-06 Issue:6-7 Volume:9 Page:445-454
ISSN:0094-5765
Container-title:Acta Astronautica
language:en
Short-container-title:Acta Astronautica

Author:

Schmitt Denis,Lourme Daniel

Publisher

Elsevier BV

Subject

Aerospace Engineering

Reference6 articles.

1. Theory of combustion instability in liquid propellant rocket motors;Crocco;AGARDograph,1956

2. Behaviour of supercritical nozzles under three-dimensional oscillatory conditions;Crocco;AGARDograph,1967

3. Transverse combustion instability in liquid propellant rocket motors;Crocco;ARS J.,1962

4. Velocity effects in transverse mode liquid propellant rocket combustion instability;Reardon;AIAA J.,1964

5. Liquid propellant rocket combustion instability;Haarje;NASA SP-194,1972

Cited by 4 articles. 订阅此论文施引文献订阅此论文施引文献，注册后可以免费订阅5篇论文的施引文献，订阅后可以查看论文全部施引文献

1. Nonlinear Studies of Low-Frequency Combustion Stabilities;Mathematical Modeling in Combustion and Related Topics;1988

2. Experiments on stability of liquid propellant rocket motors;23rd Joint Propulsion Conference;1987-06-29

3. Experimental characterization of the spray originating from an impinging-jet injector in a liquid-rocket engine;Acta Astronautica;1984-07

4. Les moyens necessaires a l'etude fondamentale des instabilites de combustion d'un moteur biliquide;Acta Astronautica;1983-12

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